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Figure 9.5 shows that the change in AOC is smallest when all SCA heads are active
(black, 57.8% of epochs), and largest when both spacecraft operate on one head only
(red, 33.7% of epochs). Not conforming with the results from section 9.3.2, the change
is almost identical when one SCA head is inactive on GRACE-B only (orange, 5.27%
of epochs), as when GRACE-A is the sole spacecraft operating with one SCA head
(green, 3.2% of epochs).
9.3.4 Estimated Antenna Phase Centre Vectors
In the least squares adjustment for the Stokes coefficients, the KBR antenna phase
centre vectors for GRACE-A and GRACE-B were co-estimated (compare section 6.4.2).
The following results are based on the APC estimates obtained from within the
determination of the stochastic model. The estimated APC vector for one satellite s
is
cˆs=cs+∆cˆs , (9.3.2)
wherecs is the a priori calibrated KBR APC for the satellite, which was used as a Taylor
point in the estimation. The in-orbit calibrated APC coordinates obtained from the
GRACE sequence of events file are given in table 9.1. Alongside the calibrated values,
the formal errors from the adjustment for∆cˆare given for an example month of good
data quality. The formal errors are given for the adjustment using the old stochastic
model, the model including AOC covariance matrices, and the TLS solution. Note that
the formal errors do not vary much between months, and that they are small, on the
orderofsomemicrometres.Theestimatedimprovements∆cˆ to thepublishedcalibrated
APCs for the processed time series are displayed in fig. 9.6. Results for the period
after August 2016, which are very strongly affected by the disabled accelerometer on
GRACE-B (Flechtner, 2016), are excluded from the analysis in this section.
Table 9.1: Calibrated KBR APC coordinates and formal errors from their estimation for
April 2008.
Calibrated value σOld model σIncl. AOC σWith TLS
GRACE-A
xAPC 1.445m 5.241µm 5.308µm 5.437µm
yAPC −0.423µm 0.018µm 0.018µm 0.018µm
zAPC 2.278µm 0.021µm 0.021µm 0.020µm
GRACE-B
xAPC 1.444m 10.062µm 10.052µm 10.095µm
yAPC 0.576µm 0.031µm 0.030µm 0.030µm
zAPC 3.304µm 0.041µm 0.041µm 0.041µm
Chapter9 Co-Estimation of Orientation
Parameters136
Contributions to GRACE Gravity Field Recovery
Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
- Titel
- Contributions to GRACE Gravity Field Recovery
- Untertitel
- Improvements in Dynamic Orbit Integration, Stochastic Modelling of the Antenna Offset Correction, and Co-Estimation of Satellite Orientations
- Autor
- Matthias Ellmerr
- Verlag
- Verlag der Technischen Universität Graz
- Ort
- Graz
- Datum
- 2018
- Sprache
- englisch
- Lizenz
- CC BY 4.0
- ISBN
- 978-3-85125-646-8
- Abmessungen
- 21.0 x 29.7 cm
- Seiten
- 185
- Schlagwörter
- Geodäsie, Gravitation, Geodesy, Physics, Physik
- Kategorien
- Naturwissenschaften Physik
- Technik